[PDF] Aerothermodynamics Of Gas Turbine And Rocket Propulsion eBook

Author : Gordon C. Oates
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 480 pages
File Size : 13,40 MB
Release : 1997
Category : Science
ISBN :

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This seminal book on gas turbine technology has been a bestseller since it was first published. It now includes a comprehensive set of software programs that complement the text with problems and design analyses. Software topics included are atmosphere programs, quasi-one-dimensional flow programs (ideal constant-area heat interaction, adiabatic constant-area flow with friction, rocket nozzle performance, normal shock waves, oblique shock waves), gas turbine programs (engine cycle analysis and engine off-design performance), and rocket combustion programs (Tc and PC given, He and PC given, isentropic expansion).

Author : Paul G. A. Cizmas
Publisher :
Page : 488 pages
File Size : 27,87 MB
Release : 2021-11-24
Category : Science
ISBN : 1108575595

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Get up to speed with this robust introduction to the aerothermodynamics principles underpinning jet propulsion, and learn how to apply these principles to jet engine components. Suitable for undergraduate students in aerospace and mechanical engineering, and for professional engineers working in jet propulsion, this textbook includes consistent emphasis on fundamental phenomena and key governing equations, providing students with a solid theoretical grounding on which to build practical understanding; clear derivations from first principles, enabling students to follow the reasoning behind key assumptions and decisions, and successfully apply these approaches to new problems; practical examples grounded in real-world jet propulsion scenarios illustrate new concepts throughout the book, giving students an early introduction to jet and rocket engine considerations; and online materials for course instructors, including solutions, figures, and software resources, to enhance student teaching.

Author : F. Whittle
Publisher : Elsevier
Page : 276 pages
File Size : 47,24 MB
Release : 2013-10-22
Category : Science
ISBN : 1483293211

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For the first time simplified methods of dealing with gas turbine thermal cycles, and further theoretical innovations, have been embodied into a concise textbook. All the major aspects of the subject are covered in a comprehensive and lucid manner. Examples are included for greater clarity

Author : Jack D. Mattingly
Publisher : American Institute of Aeronautics and Astronautics Incorporated
Page : 0 pages
File Size : 17,19 MB
Release : 2016
Category : Aircraft gas-turbines
ISBN : 9781624103711

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Elements of Propulsion: Gas Turbines and Rockets, Second Edition provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers. Textbook coverage has been revised and expanded, including a new chapter on compressible flow. Design concepts are introduced early and integrated throughout. Written with extensive student input, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles.

Author : Jack D. Mattingly
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 0 pages
File Size : 14,20 MB
Release : 2005
Category : Aircraft gas-turbines
ISBN : 9781563477782

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This text provides an introduction to gas turbine engines and jet propulsion for aerospace or mechanical engineers. The text is divided into four parts: introduction to aircraft propulsion; basic concepts and one-dimensional/gas dynamics; parametric (design point) and performance (off-design) analysis of air breathing propulsion systems; and analysis and design of major gas turbine engine components (fans, compressors, turbines, inlets, nozzles, main burners, and afterburners). Design concepts are introduced early (aircraft performance in introductory chapter) and integrated throughout. Written with extensive student input on the design of the book, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, and gas turbine engine principles.